System and method for analyzing and imaging three-dimensional volume data sets

ABSTRACT

A system and method is provided for analyzing and imaging three-dimensional volume data sets. In one embodiment of the invention, a ribbon section is produced which may include a plurality of planes projected from a polyline. The polyline may include one or more line segments preferably formed within a plane. The projected planes intersect the three-dimensional volume data set and the data located at the intersection may be selectively viewed. The polyline may be edited or varied by editing or varying the control points which define the polyline. In another embodiment of the present invention, a method is provided for quickly tracking a physical phenomena represented within the three-dimensional volume data set. A plurality of planes may be successively displayed in the three-dimensional volume data set from which points are digitized related to the structure of interest to create a spline curve on each plane. The area between the spline curves is interpolated to produce a surface representative of the structure of interest, which may for example be a fault plane described by the three-dimensional volume data set. In this manner, the user can more easily and effectively visualize and interpret the features and physical parameters that are inherent in the three-dimensional volume data set.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. application Ser. No.11/056,823 filed Feb. 12, 2005, which is a continuation of U.S. Pat. No.7,006,085, both of which claim the benefit of PCT/US2000/29835 filed onOct. 30, 2000, and are incorporated herein by reference.

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH

Not applicable.

FIELD OF THE INVENTION

The present invention relates generally to imaging of three-dimensional(“3D”) volume data sets. More particularly, the present inventionrelates to fast visualization and analysis of structures within 3Dvolume data sets.

BACKGROUND OF THE INVENTION

Many fields of endeavor require the analysis and imaging ofthree-dimensional (“3D”) volume data sets. For example, in the medicalfield, a CAT (computerized axial tomography) scanner or a magneticresonance imaging (MRI) device is used to produce a “picture” ordiagnostic image of some part of a patient's body. The scanner or MRIdevice generates a 3D volume data set that needs to be imaged ordisplayed so that medical personnel can analyze the image and form adiagnosis.

Three-dimensional volume data sets are also used in various fields ofendeavor relating to the earth sciences. Seismic sounding is one methodfor exploring the subsurface geology of the earth. An undergroundexplosion or earthquake excites seismic waves, similar to low frequencysound waves, that travel below the surface of earth and are detected byseismographs. The seismographs record the time of arrival of the seismicwaves, both direct and reflected waves. Knowing the time and place ofthe explosion or earthquake, the time of travel of the waves through theinterior can be calculated and used to measure the velocity of the wavesin the interior. A similar technique can be used for offshore oil andgas exploration. In offshore exploration, a ship tows a sound source andunderwater hydrophones. Low frequency (e.g., 50 Hz) sound waves aregenerated by, for example, a pneumatic device that works like a balloonburst. The sounds bounce off rock layers below the sea floor and arepicked up by the hydrophones. In this manner, subsurface sedimentarystructures that trap oil, such as faults, folds, and domes, are “mapped”by the reflected waves. The data is processed to produce 3D volume datasets that include a reflection or seismic amplitude datavalue atspecified (x, y, z) locations within a geographic space.

A 3D volume data set is made up of “voxels” or volume elements. Eachvoxel has a numeric value for some measured or calculated property,e.g., seismic amplitude of the volume at that location. One conventionalapproach to generating an image of a 3D volume data set is tocross-section the 3D volume data set into a plurality of two-dimensional(“2D”) cross-sections or slices. The image of the 3D volume data set isthen built as a composite of the 2D slices. For example, the image ofthe 3D volume data set is generated by stacking the 2D slices in order,back-to-front, and then composited into a complete image. The user seesthe image being built layer by layer as the composite grows. Althoughthe user can see the internal organization or structure of the volume asthe composite image grows, the traditional slice and composite techniqueis typically slow, particularly when very large 3D volume data sets arebeing used. Additionally, the slice and composite technique clutters theuser's field of view with extraneous information, and interferes withthe user's ability to accurately visualize and interpret featuresinherent in the 3D volume data set.

Computer software has been developed specifically for imaging 3D seismicdata sets for the oil and gas industry. Examples of such conventionalcomputer programs include VoxelGeo, available from Paradigm Geophysical,Houston, Tex., SeisWorks and EarthCube, available from Landmark GraphicsCorporation, and IESX, available from GeoQuest. Such conventionalcomputer programs have numerous deficiencies that preclude a user fromquickly and accurately visualizing and interpreting features inherent ina 3D seismic data set. Conventional computer programs for visualizingand interpreting 3D seismic data operate on the full 3D volume ofseismic data. Consequently, every time a change is made, such as achange to the transparency or opacity settings, the full 3D volume ofseismic data must be processed, and the image re-drawn. Even when suchprograms are run on highly efficient graphics supercomputers, the delayor lag in re-drawing the image is perceptible to the user. For a 3Dvolume containing 500 megabytes of seismic data, it can take on theorder of 30-45 seconds for conventional programs to re-draw the completeimage (frame rate of 0.03 to 0.02 frames per second, respectively).During the 30-45 second delay time, the mind of the user loses focus onthe feature of interest, making it difficult to completely and properlyanalyze the seismic data.

Some conventional 3D seismic interpretation programs provide thecapability to visualize and interpret a piece of the full 3D volume ofseismic data. The user identifies the coordinates of the selected piecevia a menu command. An image of the selected piece is drawn. Theselected piece can then be rotated, if desired, at that location.However, to look at a different piece of the full 3D volume of seismicdata, such as to follow a geologic feature that has been tentativelyidentified, the image must be interrupted, a new location or coordinatesfor the different piece is entered, and a new image is drawn containingthe different piece. The interruption in the displayed image makes itdifficult for the user to visualize any continuity between the twopieces of the full 3D volume of seismic data that have been imaged. Thisimpedes the user's ability to interpret and identify the geologicfeatures that are inherent in the full 3D volume of seismic data.Additionally, even though only a piece of the full 3D volume of seismicdata is being visibly displayed, conventional 3D seismic interpretationprograms continue processing the full 3D volume of seismic data to drawthe image, thereby slowing the display of the image to the user.

Conventional 3D seismic interpretation programs provide the capabilityto “auto pick” and identify points that satisfy a voxel selectionalgorithm. However, these programs typically iterate through the full 3Dvolume of seismic data to identify the points that satisfy the voxelselection algorithm. This is time consuming even on a high speedgraphics supercomputer. Additionally, conventional 3D seismicinterpretation programs do not provide the capability to directly deletefrom the collection of picked voxels. The only way to “eliminate” pointsfrom the collection of picked voxels using conventional 3D seismicinterpretation programs is to repeatedly adjust the selection criteriafor the voxel selection algorithm until the points to be eliminated falloutside of the selection criteria for the displayed points that satisfythe voxel selection algorithm. Each time the selection criteria isadjusted, the image must be interrupted. This iterative process is timeconsuming, and interferes with the visualization process of the user.

Thus, there is a need in the art for a system and method for imaging 3Dvolume data sets that overcomes the deficiencies detailed above.Particularly, there is a need for a system and method that re-drawsimages of large 3D volume data sets in response to user input at a ratesufficiently fast that the user perceives an instantaneous or real-timechange in the image, without perceptible delay or lag. There is a needfor a system and method that allows a user to interactively change thedisplayed image in a continuous manner, without interruption orperceptible delay or lag. Such a system and method would allow a user tomore quickly and accurately interpret and identify features inherent in3D volume data sets.

SUMMARY OF THE INVENTION

The present invention is directed to a system and method for analyzingand imaging 3D volume data sets using a 3D sampling probe and otherinteractive tools. In one aspect of the invention, a method and computerprogram is provided which may be stored on a storage means for imaging athree-dimensional volume data set comprising a plurality of voxels whereeach voxel comprises a three-dimensional location and a dataword. Thedataword may be representative of a physical phenomena, e.g., anamplitude signal related to a particular position within a geobody. Themethod may comprise steps such as creating at least onethree-dimensional sampling probe, wherein the three-dimensional samplingprobe is the same size or a subset of the three-dimensional volume dataset. The three-dimensional sampling probe has a probe face plane and anopposing probe face plane. Other steps may include producing a pluralityof control points in the probe face plane such that the plurality ofcontrol points define one or more lines on the probe face plane, andextending a ribbon section from the one or more lines on the probe faceplane toward the opposing probe face plane. An edge of the ribbonsection is preferably formed by the one or more lines. Another step ofthe method may include selectively imaging datawords representative ofthe physical phenomena at three-dimensional locations which intersectthe ribbon section and the three-dimensional sampling probe.

The method may further comprise steps of editing the plurality ofcontrol points on the probe face plane to thereby redefine the one ormore lines, and extending a correspondingly redefined ribbon sectionfrom the one or more lines on the probe face plane toward the opposingprobe face plane. The step of editing may further comprise functionssuch as deleting one or more of the plurality of control points,changing a location of one or more of the plurality of control points,and adding one or more control points to the plurality of controlpoints.

In a preferred embodiment, the ribbon section is perpendicular to theprobe face plane and the ribbon section may extend from the probe faceplane to the opposing probe face plane. The one or more lines formingthe edge of the ribbon section may be edited through the plurality ofcontrol points to construct a plurality of open straight lines or aclosed line geometrical figure, if desired The ribbon section ispreferably comprised of a plurality of planes. The ribbon section may ormay not be parallel with respect to each of a plurality of side faces ofthe probe.

In another embodiment of the present invention related to tracking aparticular physical phenomena, such as a geological fault, the methodmay comprise the steps of positioning the probe face plane at a firstposition within the three-dimensional volume data set and forming afirst set of control points on the probe face plane for tracking aphysical phenomena described by the three-dimensional volume data set.Another step may include interpolating between the first set of controlpoints to define a first spline curve. Other steps may include movingthe probe to a second position within the three-dimensional volume dataset, forming a second set of control points on the probe face plane fortracking the physical phenomena and interpolating there between suchthat the second set of control points define a second spline curve.Another step may include interpolating a three dimensional surfacebetween the first spline curve and the second spline curve which isrepresentative of the physical phenomena.

The method further permits displaying the interpolated surface where thesurface intersects the first set of control points and the second set ofcontrol points. It is an advantage of the present invention that thefirst spline curve, second spline curve and subsequent spline curves arecurvilinear.

Additional steps may include the reiterative process of moving the probeto a third position within the three-dimensional volume data set,forming a third set of control points on the probe face plane fortracking the physical phenomena, interpolating between the third set ofcontrol points to define a third spline curve, and interpolating betweenthe first spline curve, the second spline, and the third spline curvefor further defining the three dimensional surface representative of thephysical phenomena.

If desired, the method may further comprise steps such as editing therespresentive control points on the probe face plane at respectivepositions of the probe. Moreover, the method may include displaying acurvilinear connection (“v curves”) between respective control points atrespective positions of the probe. Another step may include displayingthe spline curves and the v-curves on the three dimensional surface. Thespline curves and the v-curves form a three dimensional grid alsorepresentative of the physical phenomena. The grid includes a pluralityof intersections between the spline curves and the v-curves. The methodmay further comprise editing the current set of control points on theprobe face plane, thereby reshaping the surface and grid between thecurrent spline curve and the prior spline curve.

Preferably the method may also include steps such as selecting one ofthe plurality of intersections to thereby reposition the probe faceplane to pass through the selected intersection. The method alsocomprises selecting one of the sets of control points to therebyreposition the probe face plane to pass through the selected set ofcontrol points.

Stated another way, an embodiment of the method may comprise steps suchas positioning the probe face plane at a plurality of positions withinthe three-dimensional volume data set, forming a set of control pointsat each of the plurality of probe face plane positions such that eachset of control points defines a related spline curve, repositioning theprobe face plane and interpolating between the plurality of splinecurves to form a three dimensional surface representative of thephysical phenomena.

FEATURES AND ADVANTAGES

It is a feature of the present invention that a ribbon section through a3D sampling probe can be created, redrawn, edited, and moved quickly andconveniently by creating a plurality of lines that are then projectedthrough the 3D sampling probe. The lines may be drawn at angles offsetfrom the coordinate system, such as an x, y, z or Cartesian coordinatesystem, of the 3D sampling probe.

It is another feature of the present invention that structures in a 3Ddata volume set, such as for instance geological structures, can bequickly mapped by selecting points of interest at a plurality oflocations in the 3D sampling probe, which points may then beinterpolated to produce a grid or surface related to the structure. Thegrid may be quickly edited and the probe may be moved to various pointson the surface by selecting grid intersections.

It is yet another feature of the present invention that, as a userinteractively moves a 3D sampling probe through a 3D volume data set,the image on the surfaces of the 3D sampling probe is re-drawn “on thefly” so that the user perceives the image changing in real-time withmovement of the 3D sampling probe. Similarly, as a user interactivelymoves a 3D sampling probe through a 3D volume data set, the 3D samplingprobe is volume rendered with varying degrees of transparency “on thefly” so that the user perceives the image changing in real-time withmovement of the 3D sampling probe.

It is a further feature of the present invention that a user caninteractively change the shape or size of a 3D sampling probe so thatthe image on the surfaces of the 3D sampling probe is re-drawn “on thefly” so that the user perceives the image changing in real-time with thechange in shape or size of the 3D sampling probe. Similarly, a user caninteractively change the shape or size of a 3D sampling probe so thatthe 3D sampling probe is volume rendered with varying degrees oftransparency “on the fly” so that the user perceives the image changingin real-time with the change in shape or size of the 3D sampling probe.

It is yet a further feature of the present invention that a user caninteractively rotate a 3D sampling probe so that the image on thesurfaces of the 3D sampling probe is re-drawn “on the fly” so that theuser perceives the image changing in real-time with the rotation of the3D sampling probe. Similarly, a user can interactively rotate a 3Dsampling probe so that the 3D sampling probe is volume rendered withvarying degrees of transparency “on the fly” so that the user perceivesthe image changing in real-time with the rotation of the 3D samplingprobe.

It is yet a further feature of the present invention that an eraser 3Dsampling probe can be created and manipulated by the user to directlydelete from an image selected points that fall within a certaindatavalue range.

It is an advantage of the present invention that a user can manipulate a3D sampling probe to interactively traverse a 3D volume data set tocontinuously follow and image a feature.

It is a further advantage of the present invention that a user caninteractively change the displayed image in a continuous manner, withoutinterruption or perceptible delay or lag. This allows a user to morequickly and accurately interpret and identify features inherent in 3Dvolume data sets.

It is yet a further advantage of the present invention that the 3Dsampling probes can be interactively re-shaped by the user to match theshape of geologic features, thereby enabling the user to bettervisualize and define the extent of geologic features.

A still further advantage of the present invention is that it can beused to visualize and interpret large volumes of 3D seismic data. Thepresent invention can be used to quickly and accurately identifydrilling sites. The present invention can advantageously be used tosharply reduce 3D seismic project cycle times, to boost production fromexisting wells, and to locate additional reserves.

BRIEF DESCRIPTION OF THE FIGURES

The present invention is described with reference to the accompanyingdrawings. In the drawings, like reference numbers indicate identical orfunctionally similar elements. Additionally, the left-most digit(s) of areference number identifies the drawing in which the reference numberfirst appears.

FIG. 1 shows one embodiment of a software or program structure forimplementing the present invention;

FIG. 2 shows a block diagram of one embodiment of the 3D sampling probeprogram of the present invention;

FIG. 3 shows a curve illustrating opacity as a function of datavalue;

FIG. 4 shows a flow diagram illustrating one embodiment for implementingthe present invention;

FIG. 5 shows a flow diagram of one embodiment for changing a defaultprobe;

FIG. 6 shows a flow diagram of one embodiment for creating additionalprobes;

FIG. 7 shows a flow diagram of one embodiment for moving a probe;

FIG. 8 shows a flow diagram of one embodiment for re-shaping a probe;

FIG. 9 shows a flow diagram of one embodiment for rotating a probe in 3Dspace;

FIG. 10 shows a flow diagram of one embodiment for rotating a probewhile fixed in space;

FIG. 11 shows a flow diagram of one embodiment for carrying out autopicking or seed selection;

FIG. 12 shows one embodiment of a computer system suitable for use withthe present invention;

FIG. 13 shows an alternate embodiment of a computer system suitable foruse with the present invention;

FIG. 14 shows further detail of an exemplary computer system suitablefor use with the present invention;

FIG. 15 illustrates three opaque probes of the present invention, withtwo of the probes intersecting each other;

FIG. 16 illustrates three probes of the present invention, a data probe,a transparent cut probe, and a volume-rendered probe;

FIG. 17 illustrates a ribbon section according to the present inventionin the shape of a star;

FIG. 18 shows a block diagram of a system for producing the ribbonsection of FIG. 17;

FIG. 19 illustrates a three dimensional grid and three dimensionalsurface representative of a physical phenomena described by a 3-D volumedata set according to the present invention; and

FIG. 20 shows a block diagram of a system for producing the grid andsurface of FIG. 19.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Overview

The present invention is directed to a system and method for analyzingand imaging three-dimensional (“3D”) volume data sets using a 3Dsampling probe. 3D volume data sets comprise “voxels” or volumeelements. Each voxel is a sample or point within a volume. Each voxelcan be expressed in the form (x, y, z, datavalue) where “x, y, z”identifies the 3D location of the point within the volume, and“datavalue” is the value of some measured or calculated attribute orphysical parameter at the specified point within the volume. Forexample, a 3D volume data set suitable for use with the presentinvention is 3D seismic data. Each voxel in a 3D seismic data can beexpressed as (x, y, z, amplitude), with amplitude corresponding to theamplitude of reflected sound waves at the specified (x, y, z) location.

Any form of information that can be expressed in the voxel form (x, y,z, datavalue) is suitable for use with the present invention. Inaddition to seismic data, examples from the oil and gas industry includeinformation from closely spaced well logs, gravity and magnetic fields,remote sensing data, and sidescan sonar image data. Other geologic orphysical information could also include temperature, pressure,saturation, reflectivity, acoustical impedance, and velocity.

Another application for the present invention is for mining. Forexample, the present invention can be used to visualize and interpretgeologic and geophysical data to locate mining sites, to locate andtrack deposits to be mined, or to locate and track geologic featuressuch as faults that would affect mining operations. The presentinvention also has application for clean up of toxic, hazardous, orother types of waste. For example, the present invention can be used tovisualize and interpret data representing the geographic extent anddistribution of the waste at a particular site. Such visualization andinterpretation is useful for prioritizing clean up at various sites, andfor developing a clean-up plan for a particular site.

The present invention can also be used with information outside of theoil and gas industry. For example, the present invention can be used foranalyzing and imaging in the medical field, where the datavalue elementof the voxel is obtained from a CAT (computerized axial tomography)scanner or a magnetic resonance imaging (MRI) procedure.

By way of explanation and example, the present invention will bedescribed in detail below using 3D seismic data as the 3D volume dataset. It is to be understood, however, that the present invention is notlimited in any way to the use of 3D seismic data.

The present invention is particularly useful as a visualization tool forinterpreting 3D seismic data. As used herein, the term “visualization”refers to the construction of a three-dimensional picture in the user'smind of physical or geologic features or physical parameters that areinherently present in 3D volume data sets. Such physical features orparameters are typically not apparent from conventional means ofprocessing 3D data sets, such as scanning a series of cross-sections ofthe 3D volume data set, because of the mental reconstruction that needsto take place in order for a user to mentally “picture” thethree-dimensional feature. Because of this mental reconstruction, it isdifficult to communicate and share among users the same 3D image. Forexample, the same 3D mental image of the terrain will not necessarily bepresent in the mind of every person that reads or analyzes atwo-dimensional (“2D”) contour map of that terrain. Through the use of3D computer graphics, users can visualize, and communicate and share,the same 3D image of 3D volume data sets. By visualizing 3D seismicdata, a team of geologists, geophysicists, and engineers can interpretthe visualized data to make exploration and production decisions, suchas drilling locations and well paths.

To accomplish the visualization function, the present invention uses thecomputer graphics techniques of texture mapping and volume rendering. By“texture map” is meant wrapping or mapping a 2D picture or image onto a2D or a 3D object. For example, a photograph of a person can be texturemapped onto a coffee cup.

The term “volume rendering” or “volume imaging” refers to drawing athree-dimensional object in a manner that conveys to a viewer thethree-dimensional nature of the object, even though the viewer may belooking at a two-dimensional display or screen. Computer graphicstechnology makes use of coloring, lighting, and shading techniques toconvey to the mind of the viewer what is high or low, behind or infront, light or dark, etc. The perspective or viewpoint can be changedso that the viewer can see all sides of the 3D object. Volume renderingtypically includes some type of transparency/opacity(opacity=1−transparency) control so that certain parts of the 3D objectare more transparent, thereby allowing a viewer to “see through” outersurfaces of an object and view its internal structures.

The present invention enables fast visualization and analysis of verylarge 3D volume data sets through the use of a “sampling probe”, alsoreferred to herein as a “probe” or “probe object”. As explained in moredetail below, the sampling probes of the present invention have numerousattributes, one of which is that they are typically created as a 3Dsub-volume of the whole 3D volume data set to be visualized andanalyzed.

A number of sampling probes can be created, shaped, sized, and movedinteractively by the user within the whole 3D volume data set. Theintersection of the sampling probe with the whole 3D volume data set istexture mapped onto the surfaces of the sampling probe, or volumerendered with varying degrees of transparency within the sampling probe.As used herein, the term “interactive” or “interactively” refers tochanging or re-drawing an image in response to user input at a ratesufficiently fast that the user perceives an instantaneous or real-timechange in the image, without perceptible delay or lag. In practice, aframe rate of at least about 10 to 15 frames per second is sufficient toachieve interactive imaging as described herein. For example, as theuser moves the sampling probe, such as by “clicking and dragging” with a“mouse”, the user perceives the texture on the surfaces of the samplingprobe changing in “real-time” with movement of the sampling probe. Asthe sampling probe changes shape, size, or location, there is nouser-perceivable delay or lag in imaging the texture, or, with varyingdegrees of transparency, volume-rendered attributes. In this manner, theuser can interactively move the sampling probes through the whole 3Dvolume, and more easily and effectively visualize and interpret thefeatures and physical parameters that are present within the geographicspace represented by the whole 3D volume data set.

System Description

The present invention may be implemented using hardware, software or acombination thereof, and may be implemented in a computer system orother processing system. One embodiment of a software or programstructure 100 for implementing the present invention is shown in FIG. 1.At the base of program structure 100 is an operating system 102.Suitable operating systems 102 include, for example, the UNIX® operatingsystem, or Windows NT® from Microsoft Corporation, or other operatingsystems as would be apparent to one of skill in the relevant art.

Menu and windowing software 104 overlays operating system 102. Menu andwindowing software 104 is used to provide various menus and windows tofacilitate interaction with the user, and to obtain user input andinstructions. Menu and windowing software 104 can include, for example,Microsoft Windows™, X Window System™ (registered trademark ofMassachusetts Institute of Technology), and MOTIF™ (registered trademarkof Open Software Foundation Inc.). As would be readily apparent to oneof skill in the relevant art, other menu and windowing software couldalso be used.

A basic graphics library 106 overlays menu and windowing software 104.Basic graphics library 106 is an application programming interface (API)for 3D computer graphics. The functions performed by basic graphicslibrary 106 include, for example, geometric and raster primitives, RGBAor color index mode, display list or immediate mode, viewing andmodeling transformations, lighting and shading, hidden surface removal,alpha blending (translucency), anti-aliasing, texture mapping,atmospheric effects (fog, smoke, haze), feedback and selection, stencilplanes, and accumulation buffer.

A particularly preferred basic graphics library 106 is OpenGL®,available from Silicon Graphics, Inc. (“SGI”), Mountain View, Calif. TheOpenGL® API is a multiplatform industry standard that is hardware,window, and operating system independent. OpenGL® is designed to becallable from C, C++, FORTRAN, Ada and Java programming languages.OpenGL® performs each of the functions listed above for basic graphicslibrary 106. Some commands in OpenGL® specify geometric objects to bedrawn, and others control how the objects are handled. All elements ofthe OpenGL® state, even the contents of the texture memory and the framebuffer, can be obtained by a client application using OpenGL®. OpenGL®and the client application may operate on the same or different machinesbecause OpenGL® is network transparent. OpenGL® is described in moredetail in the OpenGL® Programming Guide (ISBN: 0-201-63274-8) and theOpenGL® Reference Manual (ISBN: 0-201-63276-4), the entirety of both ofwhich are incorporated herein by reference.

Visual simulation graphics library 108 overlays basic graphics library106. Visual simulation graphics library 108 is an API for creatingreal-time, multi-processed 3D visual simulation graphics applications.Visual simulation graphics library 108 provides functions that bundletogether graphics library state control functions such as lighting,materials, texture, and transparency. These functions track state andthe creation of display lists that can be rendered later.

A particularly preferred visual simulation graphics library 108 is IRISPerformer, available from SGI in Mountain View, Calif. IRIS Performersupports the OpenGL® graphics library discussed above. IRIS Performerincludes two main libraries, libpf and libpr, and four associatedlibraries, libpfdu, libpfdb, libpfui, and libpfutil.

The basis of IRIS Performer is the performance rendering library libpr,a low-level library providing high speed rendering functions based onGeoSets and graphics state control using GeoStates. GeoSets arecollections of drawable geometry that group same-type graphicsprimitives (e.g., triangles or quads) into one data object. The GeoSetcontains no geometry itself, only pointers to data arrays and indexarrays. Because all the primitives in a GeoSet are of the same type andhave the same attributes, rendering of most databases is performed atmaximum hardware speed. GeoStates provide graphics state definitions(e.g., texture or material) for GeoSets.

Layered above libpr is libpf, a real-time visual simulation environmentproviding a high-performance multi-process database rendering systemthat optimizes use of multiprocessing hardware. The database utilitylibrary, libpfdu, provides functions for defining both geometric andappearance attributes of 3D objects, shares state and materials, andgenerates triangle strips from independent polygonal input. The databaselibrary libpfdb uses the facilities of libpfdu, libpf, and libpr toimport database files in a number of industry standard database formats.The libpfui is a user interface library that provides building blocksfor writing manipulation components for user interfaces (C and C++programming languages). Finally, the libpfutil is the utility librarythat provides routines for implementing tasks such as MultiChannelOption support and graphical user interface (GUI) tools.

An application program that uses IRIS Performer and OpenGL® APItypically carry out the following steps in preparing for real-time 3Dvisual simulation:

1. Initialize IRIS Performer;

2. Specify number of graphics pipelines, choose the multiprocessingconfiguration, and specify hardware mode as needed;

3. Initialize chosen multiprocessing mode;

4. Initialize frame rate and set frame-extend policy;

5. Create, configure, and open windows as required; and

6. Create and configure display channels as required.

Once the application program has created a graphical renderingenvironment by carrying out steps 1 through 6 above, then theapplication program typically iterates through a main simulation looponce per frame.

7. Compute dynamics, update model matrices, etc.;

8. Delay until the next frame time;

9. Perform latency critical viewpoint updates;

10. Draw a frame.

A 3D sampling probe program 110 of the present inventions overlaysvisual simulation graphics library 108. Program 110 interacts with, anduses the functions carried out by, each of visual simulation andgraphics library 108, basic graphics library 106, menu and windowingsoftware 104, and operating system 102 in a manner known to one of skillin the relevant art.

3D sampling probe program 110 of the present invention is preferablywritten in an object oriented programming language to allow the creationand use of objects and object functionality. A particularly preferredobject oriented programming language is C++. In carrying out the presentinvention, program 110 creates one or more probe “objects”. As notedabove, the probe objects created and used by program 110 are alsoreferred to herein as sampling probes or probes. Program 110 manipulatesthe probe objects so that they have the following attributes.

A probe corresponds to a sub-volume of a larger 3D volume. Particularly,a probe defines a sub-set that is less than the complete data set ofvoxels for a 3D volume data set. A probe could be configured to be equalto or coextensive with the complete data set of voxels for a 3D volumedata set, but the functionality of the present invention is best carriedout when the probe corresponds to a sub-volume and defines a sub-setthat is less than the complete data set of voxels for a 3D volume dataset. For example, a 3D volume data set of seismic data can contain fromabout 500 MB (megabytes) to about 10 GB (gigabytes) or more of data. A2,500 square kilometer geographic space of typical 3D seismic datacontains about 8 GB of data. A probe of the present invention for a 500MB seismic data set would preferably contain about 10-20 MB of data.

By using probes that are a sub-volume of the larger 3D volume, thequantity of data that must be processed and re-drawn for each frame ofan image is dramatically reduced, thereby increasing the speed withwhich the image can be re-drawn. The volume of a three-dimensional cubeis proportional to the third power or “cube” of the dimensions of thethree-dimensional cube. Likewise, the quantity of data in a 3D volumedata set is proportional to the third power or “cube” of its size.Therefore, the quantity of data in a sub-volume of a larger 3D volumewill be proportional to the “cubed root” (³√) of the quantity of data inthe larger 3D volume. As such, the quantity of data in a probe of thepresent invention will be proportional to the “cubed root” (³√) of thequantity of data in the 3D volume of which it is a sub-volume. By onlyhaving to process the sub-set of data that relates to the sub-volume ofthe probe, the present invention can re-draw an image in response touser input at a rate sufficiently fast that the user perceives aninstantaneous or real-time change in the image, without perceptibledelay or lag.

The probes of the present invention can be interactively changed inshape and/or size, and interactively moved within the larger 3D volume.The outside geometry or surfaces of a probe can be interactively drawnopaque or texture mapped while the probe is being changed in shapeand/or size or while the probe is being moved. The probe can be drawn orvolume rendered with varying degrees of transparency while the probe isbeing changed in shape and/or size or moved, thereby revealing theinternal structures or features of the probe.

The 3D sampling probes of the present invention can have any shape,including rectangular shapes having one or more right angles andnon-rectangular shapes having no right angles. The 3D sampling probes ofthe present invention can have orthogonal or perpendicular planes asouter surfaces (e.g., squares and rectangles), parallel planes as outersurfaces (e.g., parallelograms), or curved outer surfaces (e.g.,spheres, ovals, or cylinders). The present invention is not limited to3D sampling probes of any particular shape. The 3D sampling probes ofthe present invention can have arbitrary shapes, such as the shape of ageologic feature identified by a user. For example, as a user moves the3D sampling probe through a 3D volume of seismic data, a geologicfeature may be visualized and identified by the user. The 3D samplingprobe can be interactively re-shaped by the user to match the shape ofthe geologic feature, thereby enabling the user to better visualize anddefine the extent of that geologic feature.

A probe can be used to cut into another probe, and the intersection ofthe two probes can be imaged. A probe can be used to highlight data inaccordance with a seed selection algorithm. A probe can also be used to“erase” or delete data in accordance with a seed de-selection algorithm.These attributes will be explained in more detail below.

FIG. 2 shows a block diagram of one embodiment of 3D sampling probeprogram 110. Program 110 includes a User Interface Module (UIM) 210, aGraphics Processing Module (GPM) 220, and a Volume Sampling Module (VSM)230. A 3D volume data set is illustrated as data volume 240, alsoreferred to herein as a 3D volume. UIM 210 and GPM 220 communicate via abi-directional pathway 212. GPM 220 sends instructions and requests fordata to VSM 230 via pathway 222. UIM 210 sends instructions and requeststo VSM 230 via pathway 214. UIM 210 interacts with data volume 240through pathway 216.

Voxel data from data volume 240 is transferred to VSM 230 via datapathway 234. VSM 230 transfers data to GPM 220 via data pathway 232.Data volume 240 stores the 3D volume data set in a manner well known toone of skill in the relevant art. For example, the format for datavolume 240 can consist of two parts, a volume header followed by thebody of data that is as long as the size of the data set. The volumeheader typically contains information, in a prescribed sequence, such asthe file path (location) of the data set, size, dimensions in the x, y,and z directions, annotations for the x, y, and z axes, annotations forthe datavalue, etc. The body of data is a binary sequence of bytes, oneor more bytes per data value, that can be ordered in the followingmanner. The first byte is the datavalue at volume location (x, y,z)=(0,0,0). The second byte is the datavalue at volume location (1,0,0),the third byte is the datavalue at volume location (2,0,0), etc. Whenthe x dimension is exhausted, then the y dimension is incremented, andfinally the z dimension is incremented. The present invention is notlimited in any way to a particular data format for data volume 240.

User Interface Module 210 handles the user interface to receivecommands, instructions, and input data from the user. UIM 210 interfaceswith the user through a variety of menus through which the user canselect various options and settings, either through keyboard selectionor through one or more user-manipulated input devices, such as a“mouse”, or a 3D pointing device. UIM 210 receives user input as theuser manipulates the input device to move, size, shape, etc. a 3Dsampling probe.

The primary functions carried out by UIM 210 will now be described. UIM210 inputs from the user the identification of one or more 3D volumedata sets (represented by data volume 240) to use for imaging andanalysis. When a plurality of data volumes are used, the datavalue foreach of the plurality of data volumes represents a different physicalparameter or attribute for the same geographic space. By way of example,a plurality of data volumes could include a geology volume, atemperature volume, and a water-saturation volume. The voxels in thegeology volume can be expressed in the form (x, y, z, seismicamplitude). The voxels in the temperature volume can be expressed in theform (x, y, z,

C).

The voxels in the water-saturation volume can be expressed in the form(x, y, z, % saturation). The physical or geographic space defined by thevoxels in each of these volumes is the same. However, for any specificspatial location (x₀, y₀, z₀), the seismic amplitude would be containedin the geology volume, the temperature in the temperature volume, andthe water-saturation in the water-saturation volume.

UIM 210 inputs from the user information to create one or more 3Dsampling probes. Such information includes size, shape, and initiallocation of the probe. Such information can also include imagingattributes such as color, lighting, shading, and transparency (oropacity). By adjusting opacity as a function of datavalue, certainportions of the data volume are more transparent, thereby allowing aviewer to see through surfaces. An exemplary opacity curve 300 is shownin FIG. 3. Opacity curve 300 illustrates opacity (1−transparency) as afunction of datavalue. As would be readily apparent to one skilled inthe art, datavalues with greater opacity (less transparency) will maskthe imaging or display of datavalues with lower opacity (moretransparency). Conversely, datavalues will less opacity and greatertransparency will permit the imaging or display of datavalues withgreater opacity and lower transparency.

UIM 210 receives input from the user for sizing and shaping the 3Dsampling probes. As described in more detail below, in a preferredembodiment of the present invention, the user changes the shape and/orsize of a probe by clicking onto “sizing tabs” on the probe, and makingchanges in the dimensions of the probe in one or more directions. UIM210 receives input from the user to move the position or location of a3D sampling probe within the data volume. In a preferred embodiment, auser manipulates a mouse to “click” onto a surface of the probe to bemoved, and then moves the mouse to move the probe throughout thegeographic space defined by the data volume.

UIM 210 receives input from the user to carry out “auto picking”processes. In an auto picking process, data points (voxels) are selectedbased upon a selection algorithm. In a preferred embodiment, theselection algorithm is based upon a seed point within the 3D datavolume. The selection algorithm then selects data points that: (i)satisfy the selection criteria or algorithm (e.g., have a datavaluewithin a specified filter range); and (ii) have a connectivity with orare connected to the seed point. Through UIM 210, the user is promptedto identify a seed point within the 3D volume, and to identify a filterrange of datavalues used by the selection algorithm to “pick” theselected points. Preferably, the seed point is within one of the 3Dsampling probes.

UIM 210 also receives input from the user regarding the content of thedisplayed image. For example, the user can preferably select the contentof the displayed image. The content of the displayed image could includeonly the 3D sampling probe, i.e., its intersection with the 3D volume.Additionally, the 3D sampling probe could be displayed either with orwithout a bounding box that defines the outer geometry of the probe.Alternatively, the displayed image could include the 3D sampling probe,as well as the data that occupies the background xz, yz, and xy planes,and/or the data that occupies the 3D volume outside of the 3D samplingprobe(s) being displayed.

To carry out the foregoing functions, UIM 210 sends a request to VolumeSampling Module 230 to load or attach those 3D volume data setsidentified by the user. UIM 210 communicates via pathway 212 withGraphics Processing Module 220 that carries out the display and imaging.

The primary functions carried out by GPM 220 will now be described. GPM220 processes data for imaging of 3D sampling probes with the color,lighting, shading, transparency, and other attributes selected by theuser. To do so, GPM 220 uses the functions available through basicgraphics library 106 and visual simulation graphics library 108described above. The user can select (through UIM 210) to display onlythe one or more 3D sampling probes that have been created.Alternatively, the user can select to display one or more 3D samplingprobes, as well as the 3D data volume outside of the probes, i.e. voxelswithin the 3D volume that do not intersect any of the 3D sampling probesthat are being displayed. 3D sampling probes that are being displayedare referred to herein as “active probes”.

GPM 220 processes the re-shaping and move requests that are received byUIM 210 from the user. GPM 220 draws the re-shaped 3D sampling probe inaccordance with the user-selected attributes (color, lighting, shading,transparency, etc.). As the user inputs a change in shape for a 3Dsampling probe, the image with selected attributes is re-drawnsufficiently fast to be perceived as real-time by the user. Similarly,GPM 220 draws the 3D sampling probe in the new position or location inaccordance with the user-selected attributes (color, lighting, shading,transparency, etc.). As the user moves the 3D sampling probe through the3D volume, the image of the 3D sampling probe with selected attributesis re-drawn sufficiently fast to be perceived as real-time by the user.

GPM 220 processes “auto picking” requests that are received by UIM 210.GPM 220 will image selected points within the 3D volume in accordancewith the selection algorithm. Alternatively, GPM 220 will “erase”selected points within the 3D volume in accordance with the selectionalgorithm.

To carry out the foregoing functions, GPM 220 communicates via pathway212 with UIM 210 so that the information requested by the user is imagedor displayed with the selected attributes. GPM 220 obtains the neededdata from data volume 240 by sending a data request via pathway 222 toVolume Sampling Module (VSM) 230.

The primary function of VSM 230 is to extract the appropriate data fromdata volume 240 at the request of GPM 220. VSM 230 receives requests fordata from GPM 220 via pathway 222. VSM 230 extracts the required datafrom data volume 240 and transfers the data to GPM 220 via data pathway232 for processing and display. VSM 230 also receives instructions fromUIM 210 via pathway 214 to load or attach the 3D data volumes identifiedby the user.

Turning now to FIG. 4, a flow diagram 400 illustrating one embodimentfor implementing the present invention is shown. A start up orinitialization process is shown in a step 402. In step 402, the userspecifies the one or more data volumes (240) to be used. The specified3D volume data sets are loaded from disk into main memory (a descriptionof hardware suitable for carrying out the present invention will bedescribed in more detail below). A default 3D sampling probe is created,and drawn. The default 3D sampling probe is a sub-volume of thespecified 3D volume(s) of arbitrary size and shape. The presentinvention is not limited to any particular size or shape for the default3D sampling probe.

By way of example of the present invention, the default 3D samplingprobe can be a square (having equal dimensions in the x, y, and zdirections). To draw the square default 3D sampling probe, the boundinggeometry is first drawn with one edge of the bounding geometry locatedon the z axis. Data is then extracted from data volume 240 by VSM 230 todraw the image of the intersection of the square default 3D samplingprobe with the 3D volume (data volume 240). Particularly, data isextracted that corresponds to the intersection of the square default 3Dsampling probe with the 3D volume in the xz, yz, and xy planes. Thisdata is then sent by VSM 230 to GPM 220 so that it can be texture mappedonto the planes of the bounding box to provide an image of the squaredefault 3D sampling probe.

In one embodiment of the present invention, the data that occupies thebackground xz, yz, and xy planes themselves, as well as the data thatoccupies the 3D volume outside of the default 3D sampling probe, arealso imaged or displayed (in addition to the default 3D sampling probe)during start up step 402. Alternatively, start up step 402 can becarried out so that the data that occupies the background xz, yz, and xyplanes, or the data that occupies the 3D volume outside of the default3D sampling probe, is not displayed or imaged. Preferably, the presentinvention is carried out so that the user can selectively display, ornot display, the data that occupies the background xz, yz, and xyplanes, as well as the data that occupies the 3D volume outside of theactive probes.

In a step 404, UIM 210 is waiting to respond to user input or request.User input is received through a user input device suitable for use witha computer, including but not limited to, a keyboard, mouse, joystick,trackball, rollerball, roller point, or other type of suitable pointingdevice, etc. Preferably, the user input device comprises a mouse orother similar device that enables the user to “click” on a particulardisplayed image, and “drag” that displayed image to another location.Such a user input device allows a user to move and re-shape displayedprobes. Such a user input device also allows a user to activatedrop-down menus, and to select the various options for the color,shading, lighting, and transparency attributes. A keyboard can also beused for entering information relating to the selected attributes.

Reference numeral 406 refers generally to a plurality of functions thatcan be carried out by the present invention. These functions can becarried out individually or simultaneously, depending upon input fromthe user. For example, a probe can be moved (function 430) and rotated(function 450) simultaneously. While the functions identified byreference numeral 406 are being carried out, the image of the 3Dsampling probes is being re-drawn sufficiently fast to be perceived asreal-time by the user. Each of the functions identified by referencenumeral 406 will now be described.

If a user wants to change the default probe, then function 410 iscarried out. The steps for carrying out function 410 are shown in FIG. 5by way of flow diagram connector 5A. In a step 502, the changes to thedefault probe are input by UIM 210 from the user. For example, thechanges to the default probe can be to the shape or size, the location,or the attributes such as color, shading, lighting, and transparency.

In a step 504, UIM 210 sends a request to GPM 220 to draw the changeddefault probe. In a step 506, GPM 220 requests data for the changeddefault probe from VSM 230. In making this request, GPM 220 would invokefunction 430 if it was necessary to move the default probe, function 440to re-shape the default probe, and functions 450 or 460 to rotate thedefault probe. The foregoing functions will be described in more detailbelow.

The data that will be extracted from data volume 240 by VSM 230 inresponse to the request made by GPM 220 in step 506 will depend uponattributes that have been selected by the user. If the opacity settingsselected by the user are such that all datavalues are opaque, then thedata extracted by VSM 230 will be limited to the surfaces of the changeddefault probe. Because of the selected opacity, it will not be possiblefor the user to see inside the changed default probe, so only the datacorresponding to the surfaces or outside of the changed default probewill be extracted by VSM 230. In a step 508, GPM 220 processes the dataextracted by VSM 230 for the surfaces of the changed default probe, anddraws the changed default probe by texture mapping onto the surfaces inaccordance with the attributes selected by the user. By extracting onlythe data that can be seen by the user, the image of the changed defaultprobe can be drawn more quickly because less data needs to be processed,i.e., the data corresponding to the “inside” of the changed defaultprobe is not processed.

Alternatively, if the opacity settings selected by the user are suchthat some of the datavalues are opaque and some of the datavalues aretransparent, then the data extracted by VSM 230 will include the datacorresponding to the entire volume of the changed default probe. Becauseof the selected opacity and transparency, it will be possible for theuser to see inside the changed default probe, so data corresponding tothe entire volume of the changed default probe will be extracted by VSM230. In such a situation, GPM 220 processes the data extracted by VSM230 in step 508, and draws the changed default probe by volume renderingin accordance with the attributes selected by the user.

If a user wants to create additional probes, then function 420 iscarried out. The present invention is not limited to any particularnumber of active probes. The steps for carrying out function 420 areshown in FIG. 6 by way of flow diagram connector 6A. In a step 602, theshape, size, location, attributes, etc. for the additional probes areinput by UIM 210 from the user. In a step 604, UIM 210 sends a requestto GPM 220 to draw the additional probes.

In a step 606, GPM 220 requests data for the additional probes from VSM230. In a manner similar to that described above for changing thedefault probe, the data that is extracted from 3D or data volume 240 byVSM 230 will depend upon the opacity selected by the user for theadditional probes. If the opacity settings selected by the user are suchthat all datavalues for the additional probes are opaque, then the dataextracted by VSM 230 will be limited to the surfaces of the additionalprobes. Alternatively, if the opacity settings selected by the user forthe additional probes are such that some of the datavalues are opaqueand some of the datavalues are transparent, then the data extracted byVSM 230 will include the data corresponding to the entire volumes of theadditional probes. In this manner, the additional probes can be drawnmore quickly by minimizing the quantity of data that must be processed.

In a step 608, GPM 220 processes the data extracted by VSM 230 for theadditional probes, and draws the additional probes in accordance withthe attributes selected by the user, either by texture mapping onto thesurfaces of the additional probes, or by volume rendering the entirevolume of the additional probes.

If a user wants to move a probe, then function 430 is carried out. Thesteps for carrying out function 430 are shown in FIG. 7 by way of flowdiagram connector 7A. In a step 702, the new location for the probe isinput by UIM 210 from the user. In a preferred embodiment of the presentinvention, the user inputs the new location of the probe by clicking amouse or other type of suitable user input device to snap a pointer ontoa surface of the probe to be moved. The user changes the location of theprobe by moving the mouse or other suitable user input device in anydirection, thereby dragging the probe along a trajectory.

In a step 704, UIM 210 sends a move request to GPM 220 to draw the probeat the new location. GPM 220 requests data for the new location of theprobe from VSM 230. In a manner similar to that described above, thedata that is extracted from data volume 240 by VSM 230 will depend uponthe opacity selected by the user for the probe being moved. If theopacity settings selected by the user are such that all datavalues forthe probe being moved are opaque, then the data extracted by VSM 230will be limited to the surfaces of the probe being moved. Alternatively,if the opacity settings selected by the user for the probe being movedare such that some of the datavalues are opaque and some of thedatavalues are transparent, then the data extracted by VSM 230 willinclude the data corresponding to the entire volume of the probe beingmoved. In this manner, the probe can be drawn at its new location morequickly by minimizing the quantity of data that must be processed.

In a step 708, GPM 220 processes the data extracted by VSM 230 for theprobe being moved, and draws the probe at its new location in accordancewith the attributes selected by the user, either by texture mapping ontothe surfaces of the probe being moved, or by volume rendering the entirevolume of the probe being moved.

As the user moves the probe, for each new location of the probe, steps702 through 708 are repeated at a rate sufficiently fast that the userperceives the image of the probe, with texture mapping or volumerendering as appropriate, changing in “real-time” with movement of theprobe. The image is being re-drawn at a frame rate sufficiently fast tobe perceived as real-time by the user.

If a user wants to re-shape a probe, then function 440 is carried out.As used herein, the term “re-shape” refers to any change in dimension ofa 3D sampling probe in any direction. The shape of a 3D sampling probecan be changed, or re-shaped, for example, by changing the size in oneor more directions, such as by changing a square probe into arectangular probe by increasing the size of the probe in the xdirection, and decreasing the size of the probe in the y direction. Asanother example, the shape of a 3D sampling probe can be changed bychanging the shape from spherical to rectangular. As yet anotherexample, a square 3D sampling probe (equal dimensions in the x, y, and zdirections) can be re-shaped in accordance with the present invention tobe a larger or smaller square-shaped probe by changing the size equallyin each of the x, y, and z directions. The re-shaped probe also has asquare shape, but as a larger or smaller square.

The steps for carrying out function 440 are shown in FIG. 8 by way offlow diagram connector 8A. In a step 802, the new shape and/or size forthe probe is input by UIM 210 from the user. In a preferred embodimentof the present invention, the user inputs the new shape of a probe byclicking a mouse or other type of suitable user input device to snap apointer onto a “sizing tab” of the probe to be re-shaped. As usedherein, a “sizing tab” refers to a designated area on a surface of theprobe. Such a designated area is preferably displayed in a color that isdifferent from the colors being used to display the features or physicalparameters of the 3D volume data set. When the pointer is snapped to thesizing tab, manipulation of the mouse or user input device changes thedimensions or proportions of the surface on which the sizing tab islocated. When the desired size or shape is reached, the user againclicks the mouse or user input device to release the pointer from thesizing tab. Sizing tabs are illustrated in FIGS. 15 and 16. The sizingtabs are the small dark squares that appear on the surfaces of theprobes, along the bounding geometry of the probes. The location of thesizing tabs is not limited to the bounding geometry of the probes. Theuser changes the shape of the probe by clicking the mouse or othersuitable user input device onto a sizing tab, moving the mouse until thesurface being changed has the desired shape, and then releasing themouse from the sizing tab. This process can be repeated, if necessary,using other sizing tabs on the probe until the probe is re-shaped to thedesired shape.

It would be readily apparent to one of skill in the relevant art how toimplement such a sizing tab for re-shaping the probes of the presentinvention. It is to be understood, however, that the present inventionis not limited to the use of sizing tabs for re-shaping probes, andother suitable methods can be used. For example, the user could selectfrom a number of pre-set shapes (e.g., squares, rectangle, cylinders,spheres) by activating a drop-down menu, or by scrolling through theshapes by repeatedly clicking a mouse.

In a step 804, UIM 210 sends a re-shape request to GPM 220 to draw there-shaped probe. In a step 806, it is determined whether more data isneeded to draw the re-shaped probe. For example, if the re-shaped probeis of a shape and size that “fits inside” the existing probe, then nomore data is needed, and processing continues at a step 810.Alternatively, if the re-shaped probe is of a shape and size that fallsat least partially outside of the existing probe, then, in a step 808,GPM 220 requests the data needed for the re-shaped probe from VSM 230.In a manner similar to that described above, the data that is extractedfrom 3D or data volume 240 by VSM 230 will depend upon the opacityselected by the user for the probe being re-shaped. If the opacitysettings selected by the user are such that all datavalues for the probebeing re-shaped are opaque, then the data extracted by VSM 230 will belimited to the surfaces of the probe being re-shaped. Alternatively, ifthe opacity settings selected by the user for the probe being re-shapedare such that some of the datavalues are opaque and some of thedatavalues are transparent, then the data extracted by VSM 230 willinclude the data corresponding to the entire volume of the probe beingre-shaped. In this manner, the probe can be drawn with its new shapemore quickly by minimizing the quantity of data that must be processed.

In step 810, GPM 220 processes the data extracted by VSM 230 for theprobe being re-shaped, and draws the probe with its new shape inaccordance with the attributes selected by the user, either by texturemapping onto the surfaces of the probe being re-shaped, or by volumerendering the entire volume of the probe being re-shaped.

As the user changes the shape of the probe, steps 802 through 810 arerepeated at a rate sufficiently fast that the user perceives the imageof the probe, with texture mapping or volume rendering as appropriate,changing in “real-time” with the changing shape of the probe. The imageis being re-drawn at a frame rate sufficiently fast to be perceived asreal-time by the user.

If a user wants to rotate a probe in 3D space, then function 450 iscarried out. In function 450, the 3D orientation, which is the same forboth the 3D volume and the probe, is changed, thereby rotating the 3Dvolume and the probe in space. The steps for carrying out function 450are shown in FIG. 9 by way of flow diagram connector 9A. In a step 902,the new 3D orientation for the 3D volume and the probe is input by UIM210 from the user. In a preferred embodiment of the present invention,the user inputs the new orientation by clicking a mouse or other type ofsuitable user input device to snap a pointer onto an axis of the probeto be rotated. Manipulation of the mouse or user input device changesthe orientation of that axis. When the desired orientation is reached,the user again clicks the mouse or user input device to release thepointer from the axis. It would be readily apparent to one of skill inthe relevant art how to implement such a change in orientation. It is tobe understood, however, that the present invention is not limited tochanging the orientation in this manner. For example, the user couldselect from a number of pre-set rotations (e.g., rotate 90° to the leftor right; rotate 45° to the left or right, etc.) by activating adrop-down menu, or by scrolling through the rotations by repeatedlyclicking a mouse.

In a step 904, UIM 210 sends a request to rotate in 3D space to GPM 220to draw the rotated probe. In a step 906, GPM 220 requests data for therotated probe from VSM 230. In a manner similar to that described above,the data that is extracted from 3D or data volume 240 by VSM 230 willdepend upon the opacity selected by the user for the probe beingrotated. If the opacity settings selected by the user are such that alldatavalues for the probe being rotated are opaque, then the dataextracted by VSM 230 will be limited to the surfaces of the probe beingrotated. Alternatively, if the opacity settings selected by the user forthe probe being rotated are such that some of the datavalues are opaqueand some of the datavalues are transparent, then the data extracted byVSM 230 will include the data corresponding to the entire volume of theprobe being rotated. In this manner, the probe can be drawn with its neworientation more quickly by minimizing the quantity of data that must beprocessed.

In step 908, GPM 220 processes the data extracted by VSM 230 for theprobe being rotated, and draws the probe with its new orientation inaccordance with the attributes selected by the user, either by texturemapping onto the surfaces of the probe being rotated, or by volumerendering the entire volume of the probe being rotated.

As the user rotates the probe in 3D space, steps 902 through 908 arerepeated at a rate sufficiently fast that the user perceives the imageof the probe, with texture mapping or volume rendering as appropriate,changing in “real-time” with the changing orientation of the probe. Theimage is being re-drawn at a frame rate sufficiently fast to beperceived as real-time by the user.

If a user wants to rotate a probe while it is fixed in 3D space, thenfunction 460 is carried out. In function 460, the 3D orientation of theprobe is rotated independently of the 3D orientation of the 3D volume,thereby rotating the probe while it is fixed in the 3D space defined bythe orientation of the 3D volume. In this manner, the background planesfor an active probe can be displayed in a fixed orientation, and theactive probe can be rotated within the background planes.

The steps for carrying out function 460 are shown in FIG. 10 by way offlow diagram connector 10A. In a step 1002, the new 3D orientation forthe probe is input by UIM 210 from the user. In a preferred embodimentof the present invention, the user selects the option to rotate whilefixed in space, for example, from a “drop-down” menu. The user theninputs the new orientation for the probe by clicking a mouse or othertype of suitable user input device to snap a pointer onto an axis of theprobe to be rotated. Manipulation of the mouse or user input devicechanges the orientation of that axis. When the desired orientation isreached, the user again clicks the mouse or user input device to releasethe pointer from the axis. It would be readily apparent to one of skillin the relevant art how to implement such a change in orientation. It isto be understood, however, that the present invention is not limited tochanging the orientation in this manner. For example, the user couldselect from a number of pre-set rotations (e.g., rotate 90° to the leftor right; rotate 45° to the left or right, etc.) by activating adrop-down menu, or by scrolling through the rotations by repeatedlyclicking a mouse.

In a step 1004, UIM 210 sends a request to rotate while fixed in spaceto GPM 220 to draw the rotated probe. In a step 1006, GPM 220 requestsdata for the rotated probe from VSM 230. In a manner similar to thatdescribed above, the data that is extracted from 3D or data volume 240by VSM 230 will depend upon the opacity selected by the user for theprobe being rotated. If the opacity settings selected by the user aresuch that all datavalues for the probe being rotated are opaque, thenthe data extracted by VSM 230 will be limited to the surfaces of theprobe being rotated. Alternatively, if the opacity settings selected bythe user for the probe being rotated are such that some of thedatavalues are opaque and some of the datavalues are transparent, thenthe data extracted by VSM 230 will include the data corresponding to theentire volume of the probe being rotated. In this manner, the probe canbe drawn with its new orientation more quickly by minimizing thequantity of data that must be processed.

In step 1008, GPM 220 processes the data extracted by VSM 230 for theprobe being rotated, and draws the probe with its new orientation inaccordance with the attributes selected by the user, either by texturemapping onto the surfaces of the probe being rotated, or by volumerendering the entire volume of the probe being rotated.

As the user rotates the probe while it is fixed in space, steps 1002through 1008 are repeated at a rate sufficiently fast that the userperceives the image of the probe, with texture mapping or volumerendering as appropriate, changing in “real-time” with the changingorientation of the probe. The image is being re-drawn at a frame ratesufficiently fast to be perceived as real-time by the user.

If a user wants to carry out an “auto picking” process, then function470 is carried out. The steps for carrying out function 470 are shown inFIG. 11 by way of flow diagram connector 11A. In a step 1102, a seedpoint within the data set of the 3D volume, and a selection criteriabased on datavalues, are input by UIM 210 from the user. Preferably theseed point is within the data set of voxels that defines a probe. Asdescribed below, such a probe is referred to herein as a seed 3Dsampling probe or an eraser 3D sampling probe. However, the seed pointcan be within the data set of voxels that defines the 3D volume, outsideof an active probe. In a preferred embodiment of the present invention,the user selects the option to execute an auto picking process, forexample, from a “drop-down” menu. The user then selects the seed pointby clicking a mouse or other type of suitable user input device to snapa pointer onto the desired seed point. The selection criteria can beinput, for example, by graphically selecting a range, or by keying inspecific numerical values. It would be readily apparent to one of skillin the relevant art how to input from the user a seed point and filterrange of datavalues.

In a step 1104, UIM 210 sends an auto picking request to GPM 220 to drawthe rotated probe. In a step 1106, GPM 220 requests selected points toimage from VSM 230. The selected points are those that are connected tothe seed point, and that have a datavalue within the selection criteria.

In step 1108, GPM 220 processes the data extracted by VSM 230 to drawthe selected points. The selected points are preferably highlighted bybeing drawn in a color different from those used to depict the featuresor physical parameters of the 3D volume data set. Alternatively, step1108 can be carried out to “erase” or delete from the image the selectedpoints.

In a similar manner, auto picking function 470 can be used to “erase” orde-select points. For example, an eraser 3D sampling probe is defined,such as by invoking function 420 to create an additional probe. A“de-selection” criteria based on datavalues is defined. Pointspreviously selected by an auto picking operation that satisfy thede-selection criteria are identified as candidates for de-selection. Asthe eraser 3D sampling probe moves through the 3D volume, thede-selected points are deleted from the image, and the image is re-drawnsufficiently fast to be perceived as real-time by the user.

Once auto picking function 470 is initiated by the user, it can becarried out simultaneously with, for example, move function 430. In thismanner, as the user moves the probe, steps 1102 through 1108 (and steps702 through 708) are repeated at a rate sufficiently fast that the userperceives the image of the probe, with the selected points, changing in“real-time” with the changing location of the probe. As the probe ismoved, the selected points can be highlighted by being drawn in asuitable color, thereby having the auto-picking 3D sampling probefunction as a “highlighter” as it moves through the 3D volume.Alternatively, as the probe is moved, points previously selected by anauto picking operation can be “erased” or deleted from the image,thereby having the probe function as an “eraser” or eraser 3D samplingprobe as it moves through the 3D volume. In either embodiment, the imageis being re-drawn at a frame rate sufficiently fast to be perceived asreal-time by the user.

If a user wants to create a “ribbon section,” then function 480 isperformed. The steps necessary for performing function 480 are describedfurther below in reference to FIG. 17 and by way of block diagramconnector 18A in FIG. 18.

If a user wants to create a “3D surface” representative of a physicalphenomena found within a 3D volume data set, then function 490 isperformed. The steps necessary for performing function 490 are describedfurther below in reference to FIG. 19 and by way of block diagramconnector 20A in FIG. 20.

In any event where a user desires to carry out one or more of thefunctions described above such as more probe (430), re-shape probe(440), create a ribbon section (480) and create a 3D surface (490), eachfunction can be performed independent of, or in connection with, one ormore of the other functions.

With reference now to FIG. 12, one embodiment of a computer systemsuitable for use with the present invention is shown. A graphicssupercomputer 1210 contains one or more central processing units (CPU)or processors 1212. Supercomputer 1210 contains a random access memory(RAM) 1214 that can be accessed by processors 1212. Supercomputer 1210also contains one or more graphics modules 1216 that also access RAM1214. Graphics modules 1216 execute the functions carried out byGraphics Processing Module 220, using hardware (such as specializedgraphics processors) or a combination of hardware and software. A userinput device 1218 allows a user to control and input information tographics supercomputer 1210.

A particularly preferred graphics supercomputer is an Onyx2 InfiniteReality system, available from Silicon Graphics, Inc., Mountain View,Calif., configured with eight processors, three graphics pipelines, 16GB of main memory, and 250 GB of disk memory. Such a graphicssupercomputer has a scalable, high-bandwidth, low-latency architectureto provide high speed rendering on multiple graphics pipelines. Graphicssupercomputers from other vendors, such as Hewlett-Packard Company ofPalo Alto, Calif. or Sun Microsystems of Mountain View, Calif. couldalso be used.

The graphics data forming the image to be displayed is sent fromgraphics supercomputer 1210 to a multiple-screen display system 1220 forprojection onto a screen 1230. In the embodiment shown in FIG. 12, threeprojectors are used. From the perspective of a user viewing the image onscreen 1230, the three projectors include a left projector 1240, acenter projector 1250, and a right projector 1260. Although threeprojectors are shown, the present invention is not limited to the use ofany particular number of projectors.

Projector 1240 has a projection field on screen 1230, shown generally at1242, between a point 1241 and a point 1243. Projector 1250 has aprojection field on screen 1230, shown generally at 1252, between apoint 1251 and a point 1253. Projector 1260 has a projection field onscreen 1230, shown generally at 1262, between a point 1261 and a point1263. Projection fields 1242 and 1252 have an overlap region 1244,between points 1251 and 1243. Similarly, projection fields 1262 and 1252have an overlap region 1264, between points 1261 and 1253. The image tobe displayed is divided into three (left, center, and right)over-lapping sub-images. By simultaneously projecting the threeover-lapping sub-images, the field-of-view to the user is increased overthat available, for example, on a monitor or through the use of just oneprojector. As an example, use of the three over-lapping sub-images shownin FIG. 12 increases the field-of-view to approximately 160°. Overlapregions 1244 and 1264 are each approximately 5.3°. Multiple-screendisplay system 1220 accounts for overlap regions 1244 and 1264 in awell-known manner to edge-blend the images of the three projectors toform one seamless image on screen 1230. Suitable display and projectorsystems are available from SEOS, London, England, such as the Barcoprojector units.

FIG. 13 shows an alternate embodiment of a computer system suitable foruse with the present invention. In the embodiment shown in FIG. 13,graphics supercomputer 1210 is configured with multiple processors 1212,RAM 1214, and two graphics modules 1216. Graphics workstations suitablefor use in the embodiment shown in FIG. 13 are available from SiliconGraphics, Inc. or Sun Microsystems. Each graphics module 1216 isconnected to a monitor 1320 for display. Monitor 1320 should preferablybe a color graphics monitor suitable for display of graphics such asthat shown in FIGS. 15 and 16. Preferably, one of monitors 1320 displaysthe image of the 3D sampling probes, and the other of monitors 1320displays the various menus used to operate 3D sampling probe program110. FIG. 13 also shows a keyboard 1330 and a mouse 1332 that functionas user input devices.

A computer system capable of carrying out the functionality describedherein is shown in more detail in FIG. 14. Computer system 1402 includesone or more processors, such as processor 1404. Processor 1404 isconnected to a communication bus 1406. Various software embodiments aredescribed in terms of this exemplary computer system. After reading thisdescription, it will become apparent to a person skilled in the relevantart how to implement the invention using other computer systems and/orcomputer architectures.

Computer system 1402 also includes a main memory 1408, preferably randomaccess memory (RAM), and can also include a secondary memory 1410.Secondary memory 1410 can include, for example, a hard disk drive 1412and/or a removable storage drive 1414, representing a floppy disk drive,a magnetic tape drive, an optical disk drive, etc. Removable storagedrive 1414 reads from and/or writes to a removable storage unit 1418 ina well known manner. Removable storage unit 1418, represents a floppydisk, magnetic tape, optical disk, etc. which is read by and written toby removable storage drive 1414. As will be appreciated, removablestorage unit 1418 includes a computer usable storage medium havingstored therein computer software and/or data.

In alternative embodiments, secondary memory 1410 may include othersimilar means for allowing computer programs or other instructions to beloaded into computer system 1402. Such means can include, for example, aremovable storage unit 1422 and an interface 1420. Examples of such caninclude a program cartridge and cartridge interface (such as that foundin video game devices), a removable memory chip (such as an EPROM, orPROM) and associated socket, and other removable storage units 1422 andinterfaces 1420 which allow software and data to be transferred fromremovable storage unit 1422 to computer system 1402.

Computer system 1402 can also include a communications interface 1424.Communications interface 1424 allows software and data to be transferredbetween computer system 1402 and external devices. Examples ofcommunications interface 1424 can include a modem, a network interface(such as an Ethernet card), a communications port, a PCMCIA slot andcard, etc. Software and data transferred via communications interface1424 are in the form of signals 1426 that can be electronic,electromagnetic, optical or other signals capable of being received bycommunications interface 1424. Signals 1426 are provided tocommunications interface via a channel 1428. Channel 1428 carriessignals 1426 and can be implemented using wire or cable, fiber optics, aphone line, a cellular phone link, an RF link and other communicationschannels.

In this document, the terms “computer program medium” and “computerusable medium” are used to generally refer to media such as removablestorage device 1418, a hard disk installed in hard disk drive 1412, andsignals 1426. These computer program products are means for providingsoftware to computer system 1402.

Computer programs (also called computer control logic) are stored inmain memory 1408 and/or secondary memory 1410. Computer programs canalso be received via communications interface 1424. Such computerprograms, when executed, enable computer system 1402 to perform thefeatures of the present invention as discussed herein. In particular,the computer programs, when executed, enable processor 1404 to performthe features of the present invention. Accordingly, such computerprograms represent controllers of computer system 1402.

In an embodiment where the invention is implemented using software, thesoftware may be stored in a computer program product and loaded intocomputer system 1402 using removable storage drive 1414, hard drive 1412or communications interface 1424. The control logic (software), whenexecuted by processor 1404, causes processor 1404 to perform thefunctions of the invention as described herein.

In another embodiment, the invention is implemented primarily inhardware using, for example, hardware components such as applicationspecific integrated circuits (ASICs). Implementation of such a hardwarestate machine so as to perform the functions described herein will beapparent to persons skilled in the relevant art(s).

In yet another embodiment, the invention is implemented using acombination of both hardware and software.

System Operation and Results

The operation and results of the present invention will now bedescribed, using a data volume 240 that contains seismic data(datavalues representing seismic amplitudes). The user specifies theparticular seismic data volume to be used, which is loaded from diskinto main memory. A default 3D sampling probe is drawn. The userspecifies the colors to be used for the seismic amplitudes. The degreeof transparency can also be selected. The three probes shown in FIG. 15are all opaque, with the intersection of the probes and the seismic datavolume texture mapped onto the surfaces of the probes. One of the probesis displayed with the bounding geometry shown; the other two probes aredisplayed without the bounding geometry.

FIG. 15 shows three active probes. The user has selected not to displaythe data contained in the background planes and in the remainder of theseismic data volume outside of the active probes. Two of the probesshown in FIG. 15 intersect each other, and the intersection of the twoprobes is displayed. In this manner, the user can more readily visualizeand interpret geologic features inherent in the seismic data volume. Forexample, a geologic feature, represented by a dark band between twolight bands, extends across the face of the larger intersecting probeand “turns the corner” to extend onto the face of the smallerintersecting probe perpendicular to it. The ability to move andintersect the probes with each other, and throughout the seismic datavolume, enables a user to better interpret and track the extent of sucha geologic feature.

FIG. 16 illustrates how one probe can be used to “cut” another probe tocreate a “hole” in a probe. As with FIG. 15, the user has selected notto display the data contained in the background planes and in theremainder of the seismic data volume outside of the active probes. FIG.16 illustrates that the opacity settings can be individually selected bythe user for each active probe. One of the probes shown in FIG. 16 isopaque, so that it is not possible to see through the surfaces of thisprobe. In order to see internal to this outer probe, it must be cut awayby another probe. The outer opaque probe is referred to as a “dataprobe”. A second completely transparent “cut probe” has been used to cutout a 3D sub-section of the data probe. Because the cut probe iscompletely transparent, it is not visible in FIG. 16. However, the factthat the completely transparent cut probe is present is evidenced by thefact that the opaque internal surfaces of the data probe are visible.The image of the intersection of the data probe and the cut probe is theintersecting surface internal to the data probe.

A third active probe is shown in FIG. 16. The third probe is displayedwith the bounding geometry shown. The third probe is volume renderedwith varying degrees of transparency so that the user can see throughthe outer surfaces of the probe and view geologic features within thethird probe. As shown in FIG. 16, the third probe is volume renderedpartially within the 3D sub-section of the data probe that has been cutaway by the cut probe.

The third volume-rendered probe shown in FIG. 16 also contains selectedpoints that have been selected through a seed picking process (function470). The selected points have been imaged in a manner to highlight themfor the user. The selected points are shown in FIG. 16 as connectingpoints. The seed point is illustrated in FIG. 16 by the darker sphere.

FIG. 17 illustrates one embodiment of a ribbon section 1710 in accordwith the present invention. Like the probe, ribbon sections are a 3-Dvolume visualization method for displaying data along user-definedtraverses through a 3-D volume data set within a probe. The traversescut through the 3-D volume data set somewhat like a cookie cutterthrough dough and therefore are referred to herein as cookie planes suchas cookie planes 1712 and 1714. Ribbon sections may display the 3-D datain orientations that do not necessarily conform to the orientation ofthe ordinate axis of the 3-D volume data set and/or probe. Ribbonsection 1710 is produced by the user in accord with the processdescribed herein below. The traverses or cookie planes are defined bydigitizing control points such as control points 1716, 1718, and 1720,which may be selected from a face of the probe referred to as the “probeface plane.” The user may create a transparent cut probe as describedabove to interface with an opaque ribbon section. Alternatively, theprobe can be made opaque and the ribbon section can be made transparentif desired.

The control points may be used to produce a plurality of line segmentssuch as line segments 1722, 1724, and 1726, which collectively arereferred to as polyline 1728 which is like a polygon but may or may notbe closed. Therefore, the line segments may form an open or closed lineso that a single or multiple cookie planes may be produced. In apreferred embodiment, the area of data display, i.e. the cookie planes,is projected along a direction perpendicular to the probe face plane andthe data displayed may extend to an opposing face of the probe referredto as the “opposing probe face plane.” After creating a ribbon section,the user may use the mouse controls or keyboard to select, move, drag,or grab the control points to edit the ribbon section 1710 in real timeand display different data from the 3D volume data set along the cookieplanes 1712 and 1714. In addition to editing the ribbon section 1710 toview different data from the 3D volume data set within the probe, theentire ribbon section 1710 and probe may be simultaneously moved to adifferent position in order to view different data from the 3D volumedata set outside the boundaries of the probe at its prior position.Active control point 1720 is preferably high-lighted or coloreddifferently as compared to the other control points to indicate controlpoint 1720 is in an active state for operations such as moving,deleting, or otherwise editing as discussed further below. Controlpoints may be inserted or deleted after the initial ribbon sectionconstruction. The ribbon section geometry and orientation may also besaved for future work sessions.

FIG. 18 depicts a block diagram of system 1810 for program modules in apresently preferred embodiment of the invention for producing ribbonsections at real time frame rates as discussed herein above. Probemodule 1822 provides initial context for sketching polyline 1728. Probemodule 1822 supplies user activity data such as mouse clicks orkeystrokes to cookie manager 1824. Thus, user activity data such ascreation of control points, deletion of control points, moving ofcontrol points, moving of the entire probe, and the like are insertedinto system 1810.

Cookie manager 1824 manages the user input data supplied by probe 1822.Cookie manager 1824 distributes the data, e.g. control points add, move,and delete as appropriate to both polyline module 1826 and cookie planemodule 1828. For some types of data, such as inserting a control point,cookie manager 1824 receives data from polyline module 1826 and passesthe data to cookie plane module 1828.

Polyline module 1826 manages data related to polyline 1728 and theassociated control points in conjunction with polymarker module 1832 andpolystate module 1830. Polyline 1728 is mainly provided for visualreference. Polyline module 1826 in conjunction with polystate module1830 manages the state of the control points. For instance, in theactive state, a control point can be moved or deleted. The activecontrol point, such as active control point 1720 is preferablyhighlighted. The control points may be enlarged or decreased in size foreasier viewing. Polymarker module 1832 provides visual context such ashighlighting or varied colors, for the control points so that anoperator knows which point is in the active state for moving, deleting,and otherwise editing. Polymarker module 1832 also may provide text suchas the location indication adjacent active control point 1720.

Cookie plane module 1828 provides textured geometry, which may forinstance be lithography-related for geological data, to the surface ofthe cookie planes such as cookie planes 1712 and 1714. Cookie statemodule 1834 monitors the state of the cookie planes so that in theactive state one or more cookie planes can be moved or otherwise editedwhereas in the inactive state no changes are made.

During operation of system 1810, probe module 1822 may notify cookiemanager 1824 that an event has taken place, e.g., a marker deletion,i.e., a control point deletion. Cookie manager 1824 then notifiespolyline module 1826 which deletes the marker or control point and joinsup the two surrounding lines into one line and notifies the polymarkermodule to remove the deleted marker from the list of polymarkersmaintained by polymarker module 1832. Cookie manager 1824 and cookieplane module then convert the two planes into one.

FIG. 19 illustrates one embodiment of the invention for creating a threedimensional surface representative of a physical phenomena described bya 3D volume data set such as, for example, a geological fault surface.In fact, this method has been found to easily and quickly provide 3Dvolume visualization for rapid identification and interpretation ofgeological fault surfaces. However, other types of surfaces for othertypes of data could also be quickly described from use of the method ofthe present invention. Although the method is described in more detailbelow, in general the method is used to digitize control points, such ascontrol points 1902, 1904, 1906, and 1908 along a probe face 1910.Visual examination of the textured surface of probe face 1910 permits anoperator to visually locate control points on a structure of interestsuch as a suspected fault line. Probe face 1910 is then moved, and a newset of control points are digitized. Surface 1912 is then interpolatedbetween the initial points and the new control points. The controlpoints may be easily edited or moved to more accurately define thesurface may be 1912 at a real time frame rate as discussed above. Thisprocess can be repeated until the surface interpretation is complete, atwhich time the surface 1912 can be saved.

Thus, one embodiment of the invention disclosed by FIG. 19 provides amethod of rapidly constructing a three-dimensional surface or faultfound within a 3-D volume data set. In a preferred embodiment, 3-Dprobes, as discussed above, are used. The method involves constructing aplurality of spline curves, such as spline curve 1914 on the probe face1910 which may be interactively constructed when visualizing the datadisplayed on probe face 1910. Spline curve 1914 is interpolated using analgorithm created in the same way as spline curves 1916, 1918, and 1920are interpolated. Spline curves and v-curves 1922, 1924, and 1926, areproduced to form a grid. The grid outlines the three dimensional surface1912.

For construction of the initial spline curve, such as for instancespline curve 1914, the user digitizes control points, such as controlpoints 1902, 1904, 1906 and 1908 on the probe face 1910. Markers areproduced at these control points and spline curve 1914 is interpolatedbetween the control points 1902, 1904, 1906 and 1908. Control points1902, 1904, 1906 and 1908 may be moved within probe face 1910, therebyinterpolating a new spline curve 1914. Once the probe face 1910 isselected, the other probe surfaces are made transparent for ease ofoperation. Additionally, the selected probe face 1910 may be made opaquein order to view surface 1912 through the probe face 1910.

The user then moves the probe face to 1910 to another position andselects new control points. The user may easily move back and forthbetween previously created spline curves by selecting grid intersectionssuch as intersection 1928 or 1930. As additional spline curves arecreated, the v-curves may also be smoothly and quickly interpolatedusing another algorithm. The user preferably creates a plurality ofspline curves in the same manner, and interpolation of surface 1912 isimmediately displayed at real time frame rates as discussed here above.

The user may stop the probe and move one or more control points, such ascontrol points 1902, 1904, 1906 and 1908 to adjust the position of therespective spline curve such as spline curve 1914. All other splinecurve, such as spline curves 1916, 1918, and 1920 remain the same whilesurface 1912 is smoothly interpolated between the current spline curve1914 on the probe face 1910 and the prior spline curve 1920. Theremainder of the surface 1912 remains the same unless the user moves theprove face 1910 to another spline curve such as 1920 and proceeds toedit the same thereby reshaping the surface 1912 between the currentspline curve 1920 on the probe face place 1910 and the prior splinecurve 1918.

Additional spline curves may be added between existing spline curves ifdesired. By selecting grid intersections such as grid intersections 1928or 1930, or by selecting control points on the probe face, such ascontrol points 1902, 1904, 1906 and 1908, the user may quickly move theprobe face 1910 back and forth as desired. Once a grid intersection isselected, the user may move the respective control points within theprobe face 1910 that will be displayed as indicated in FIG. 19, andsurface 1912 with its spline curves and v-curves will followinteractively. The spline curves and the v-curves may or may not bedisplayed depending on preference of the user. Preferably, only oneprobe face 1910 is displayed at a time for clarity.

FIG. 20 discloses modular system 2000 which describes the software forperforming the functions as described in connection with FIG. 19. In oneembodiment, modular system 2000 incorporates many of the same modules asused in modular system 1810 for producing a ribbon section. Thus, thedesign may permit a more general control that may effectively performboth ribbon section functions as well as surface mapping functions. Forinstance, cookie module 2018, polymarker module 2012, and polylinemodule 2014 may be used in the manner discussed above relating toproducing ribbon sections. Likewise, probe module 2010 therefore againperforms the functions as previously noted such as providing initialsketching splines such as spline 1914, which will also be observed to besimilar to the polylines discussed hereinbefore. Probe module 2010supplies user activity data such as mouse clicks and keystrokes to thevarious other modules. Cubic spline module 2016 relates to controllingfunctions for the editable surface or mapping feature such as surface1912 shown in FIG. 19. Cubic spline module 2016, spline manager module2020, spline curve module 2022, and spline surface module 2024 arefunctions that are different from those used only in creating ribbonsections. Spline manager 2020 performs a number of different functionssuch as creating or deleting surfaces, changing mode functions fromcreating a surface to editing a surface, as well as read and writefunctions. For instance, spline manager 2020 may read and write to asurface attribute file regarding attributes such as colors, showing thegrid, marker colors, and the like. Spline curve module 2022 keeps trackof the spline curves, keeps track of which spline curve may be in theediting or creating state and keeps track of changes made to the splinecurves. Spline surface module 2024 acts on the changes made forinterpolating the resulting surface changes.

By using the system and method of the present invention, geologists andgeophysicists can more quickly and accurately visualize and interpret 3Dseismic data. This sharply reduces 3D seismic project cycle time, boostsproduction from existing fields, and finds more reserves.

CONCLUSION

While various embodiments of the present invention have been describedabove, it should be understood that they have been presented by way ofexample only, and not limitation. Thus, the breadth and scope of thepresent invention should not be limited by any of the above-describedexemplary embodiments, and should be defined in accordance with thespirit of the invention including the following claims and theirequivalents.

1. A method for imaging a three-dimensional data volume, saidthree-dimensional data volume comprising a plurality of voxels, eachvoxel comprising a three-dimensional location and a dataword, saiddataword being representative of a physical phenomena, said methodcomprising; creating at least one three-dimensional sampling probe,wherein said three-dimensional sampling probe is the same size or asubset of said three-dimensional data volume, said three-dimensionalsampling probe having a probe face in a probe face plane and an opposingprobe face in an opposing probe face plane; producing a plurality ofcontrol points in said probe face plane, said plurality of controlpoints defining one or more lines on said probe face plane; extending aribbon section from said probe face plane toward said opposing probeface plane, one edge of said ribbon section being formed by said one ormore lines; and selectively imaging datawords representative of saidphysical phenomena only at three-dimensional locations which intersectsaid ribbon section and said three-dimensional sampling probe.
 2. Themethod of claim 1, further comprising: editing said plurality of controlpoints in said probe face plane to thereby redefine said one or morelines, and extending another redefined ribbon section from said probeface plane toward said opposing probe face plane.
 3. The method of claim2, wherein said step of editing further comprises: deleting one or moreof said plurality of control points.
 4. The method of claim 2, whereinsaid step of editing further comprises: changing a location of one ormore of said plurality of control points.
 5. The method of claim 2,wherein said step of editing further comprises: adding one or morecontrol points to said plurality of control points.
 6. The method ofclaim 1, wherein said ribbon section is perpendicular to said probe faceplane.
 7. The method of claim 1, wherein said ribbon section extendsfrom said probe face plane to said opposing probe face plane.
 8. Themethod of claim 1, wherein said one or more lines comprise a pluralityof straight lines.
 9. The method of claim 1, wherein said one or morelines form a closed line.
 10. The method of claim 1, wherein said ribbonsection is comprised of a plurality of planes.
 11. The method of claim1, wherein said three-dimensional probe has a plurality of side facesperpendicular to said probe face plane, said ribbon section beingnonparallel with respect to each of said plurality of side faces.
 12. Aprogram storage device readable by a machine, embodying a program ofinstructions executable by machine to perform method steps for imaging athree-dimensional data volume, said three-dimensional data volumecomprising a plurality of voxels, each voxel comprising athree-dimensional location and a dataword, said dataword beingrepresentative of a physical phenomena, said method comprising:displaying a plane within said three-dimensional data volume; producinga plurality of control points in said plane, said plurality of controlpoints defining one or more lines on said plane; extending a ribbonsection from said plane, one edge of said ribbon section being formed bysaid one or more lines; and selectively imaging said datawordsrepresentative of said physical phenomena only at three-dimensionallocations which intersect said ribbon section and said three-dimensionaldata volume.
 13. The method of claim 12, further comprising: editingsaid plurality of control points in said plane to thereby redefine saidone or more lines, and extending another redefined ribbon section fromsaid plane toward an opposing plane.
 14. The method of claim 13, whereinsaid step of editing further comprises: deleting one or more of saidplurality of control points.
 15. The method of claim 13, wherein saidstep of editing further comprises: changing a location of one or more ofsaid plurality of control points.
 16. The method of claim 13, whereinsaid step of editing further comprises: adding one or more controlpoints to said plurality of control points.
 17. The method of claim 12,wherein said ribbon section is perpendicular to said plane.
 18. Themethod of claim 12, wherein said ribbon section extends from said planeto an opposing plane.
 19. The method of claim 12, wherein said one ormore lines comprise a plurality of straight lines.
 20. The method ofclaim 12, wherein said one or more lines form a closed line.
 21. Themethod of claim 12, wherein said ribbon section is comprised of aplurality of planes.
 22. The method of claim 12, wherein said plane is aprobe face plane of a three-dimensional probe which has a plurality ofside faces perpendicular to said probe face plane, said ribbon sectionbeing oriented so as not to be parallel to at least one of saidplurality of side faces.